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Airbus A220-300 vs. McDonnell Douglas DC-10-30

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A220-300

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DC-10-30

Price (USD)
$91 Million$25 Million
First Flight
20151972
Body Type
Narrow-bodyWide-body
Length
38 m127 ft
55 m181 ft
Wingspan
35 m115 ft
50 m165 ft
Wing Area
112 m²1,208 ft²
338 m²3,646 ft²
Fuselage Width
3 m11 ft
6 m19 ft
Height
11 m37 ft
17 m57 ft
Max Takeoff Weight
71,900 kg158,513 lbs
251,744 kg555,001 lbs
Number of Engines
23
Engine Options
Pratt & Whitney PW1500GGeneral Electric CF6
Max Thrust Per Engine
103 kN23,000 lbf
226 kN51,000 lbf
Max Total Thrust
207 kN46,000 lbf
680 kN102,000 lbf
Fuel Capacity
21,510 l5,682 gal
137,509 l36,326 gal
Range
6,297 km3,400 nm
9,600 km5,184 nm
Cruise Speed
870 km/h541 mph
908 km/h564 mph
Typical Seating
150 pax270 pax
Max Seating
160 pax380 pax

What Are the Differences Between the Airbus A220-300 and McDonnell Douglas DC-10-30

Airbus A220-300 vs McDonnell Douglas DC-10-30 Size Comparison

  • At 55.40 meters, the McDonnell Douglas DC-10-30 is 16.70 meters longer than the Airbus A220-300.
  • With a wingspan of 50.40 meters, the McDonnell Douglas DC-10-30 is 15.30 meters wider from wingtip to wingtip.
  • The Airbus A220-300 and McDonnell Douglas DC-10-30 have heights of 11.50 meters and 17.60 meters respectively - making the McDonnell Douglas DC-10-30 6.10 meters taller.

Airbus A220-300 vs McDonnell Douglas DC-10-30 Range

  • McDonnell Douglas DC-10-30’s range of 9,600 kilometers is greater than Airbus A220-300’s range of 6,297 kilometers. Therefore, the McDonnell Douglas DC-10-30 can fly nonstop approximately 3,303 kilometers further.
  • The McDonnell Douglas DC-10-30 can hold 36,326 gallons of fuel, which is 30,644 gallons more than the Airbus A220-300’s tank capacity of 5,682 gallons.

Airbus A220-300 vs McDonnell Douglas DC-10-30 Seating

  • In a typical seating configuration, the McDonnell Douglas DC-10-30 can accommodate 270 passengers, which is about 120 passengers more than Airbus A220-300’s seating capacity.
  • The McDonnell Douglas DC-10-30’s max seating capacity is 380 passengers, compared to 160 passengers of the Airbus A220-300.

About the Airbus A220-300

The Airbus A220-300, an evolution of the A220-100 and initially known as the Bombardier CS300, is a narrow-body, twin-engine jetliner. It was designed to cater to the medium-range, single-aisle market segment. The A220-300, with its first flight in 2015, entered commercial service in 2016. It represents an expansion of the A220 aircraft family, offering enhanced capacity and range compared to its predecessor.

Featuring a length of 126.9 feet (38.7 meters) and a wingspan of 115.2 feet (35.1 meters), the A220-300 is slightly larger than the A220-100, accommodating up to 160 passengers in a standard two-class configuration. This increase in size allows airlines to serve higher passenger volumes on similar route profiles as the A220-100. Like its predecessor, the A220-300 is constructed using advanced materials, primarily composites, and innovative aluminum-lithium alloys, contributing to a lighter overall structure. This design approach results in enhanced fuel efficiency and reduced operational costs. The aircraft is powered by Pratt & Whitney PW1500G turbofan engines, delivering a thrust of up to 46,000 lbf, which supports a maximum takeoff weight of around 146,000 lbs. The A220-300's range extends to approximately 3,400 nautical miles, making it suitable for a broad spectrum of regional and medium-haul routes. The A220-300's cabin design focuses on passenger comfort, offering a wider seat and aisle configuration compared to many other aircraft in its class. The advanced avionics and Airbus's fly-by-wire system featured in the cockpit align the A220-300 with modern technological standards in aviation.

Airlines worldwide have incorporated the A220-300 into their fleets, valuing its balance of size, range, and efficiency. Operators such as AirBaltic, which was the launch customer, have utilized the aircraft for its flexibility, deploying it on diverse route networks that encompass both short and medium-haul operations. The Airbus A220-300's role in the commercial aviation market is underscored by its adaptation to current airline requirements. It offers an alternative to larger narrow-body aircraft, providing airlines with a versatile option for varying passenger demand and route structures.

As the aviation industry continues to evolve, the A220-300 stands as a testament to the ongoing shift towards more efficient, versatile aircraft. Its presence in the fleets of global airlines reflects the industry's focus on operational efficiency, passenger comfort, and environmental considerations.

About the McDonnell Douglas DC-10-30

The McDonnel Douglas DC-10-30, is a wide-body trijet airliner designed for long-haul commercial flights. As a member of the DC-10 series, the DC-10-30 was developed to extend the range and capacity of its predecessors, meeting the growing demands of global air travel. The -10-30 was a later, longer range model, and turned out to be the most variant produced. In addition to being a popular passenger aircraft, the DC-10 was also extensively used in the freight industry during its peak.

One of the DC-10's most distinctive features is its three engine configuration, with two engines mounted under the wings and a third engine at the base of the vertical stabilizer. This design was a key differentiator from other wide-body airliners of its time, such as the Boeing 747. The DC-9 made its first flight on August 29, 1970, and was introduced to the commercial aviation market on August 5, 1971 with American Airlines.

Measuring 55.4 meters (181.6 feet) in length, the DC-10-30 was among the larger aircraft of its time, capable of operating on transatlantic and transpacific routes. The aircraft features a wingspan of 50.4 meters (165.3 feet), which supports its long-range flight capabilities and stability at high altitudes. Equipped to hold over 137,500 liters (36,320 US gallons) of fuel, the DC-10-30 was designed for extended range missions, offering a maximum range of 9,600 kilometers (5,184 nautical miles). This capability enabled airlines to operate non-stop intercontinental flights over vast distances. The aircraft's propulsion system consists of 3 GE CF6-50C engines capable of delivering a combined thrust of 680.6 kN (102,000 lbf), providing the power needed for long-haul flights carrying a full complement of passengers and cargo. The DC-10-30's cruise speed of 908 km/h (564 mph) further underscores its efficiency in covering great distances swiftly.

The typical configuration for the DC-10-30 seats up to 270 passengers. Some airliners opted for higher density layouts including 3-4-2, 2-5-2, and 3-3-3. In the market for wide-body aircraft, the McDonnel Douglas DC-10-30 competed with other long-range airliners like the Lockheed L-1011 TriStar and the Boeing 747. The DC-10-30's introduction was a significant contribution to the wide-body aircraft segment, providing airlines with a versatile option for long-haul, high-capacity routes. Prominent operators of the DC-10-30 included airlines such as Continental Airlines, Garuda Indonesia, and Northwest Airlines. Other notable carriers were KLM, British Airways, Iberia, Lufthansa, and Malaysia Airlines.

The McDonnel Douglas DC-10-30's production and operational history reflect its role as a key player in the evolution of long-haul air travel. Its design, performance, and capacity made it a vital asset in the fleets of global airlines, contributing to the expansion and accessibility of international air travel during a critical period of growth in commercial aviation.

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Values shown may not be 100% accurate, as some metrics are averages or only represent certain production years and configurations. Engine specs are based on the best options available.

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